US2503016A - Lubricant scavenging pump means - Google Patents

Lubricant scavenging pump means Download PDF

Info

Publication number
US2503016A
US2503016A US548254A US54825444A US2503016A US 2503016 A US2503016 A US 2503016A US 548254 A US548254 A US 548254A US 54825444 A US54825444 A US 54825444A US 2503016 A US2503016 A US 2503016A
Authority
US
United States
Prior art keywords
pump
oil
engine
gears
gases
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US548254A
Inventor
Walter L Weeks
Charles A Stewart
William H Holmes
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wright Aeronautical Corp
Original Assignee
Wright Aeronautical Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wright Aeronautical Corp filed Critical Wright Aeronautical Corp
Priority to US548254A priority Critical patent/US2503016A/en
Application granted granted Critical
Publication of US2503016A publication Critical patent/US2503016A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16NLUBRICATING
    • F16N13/00Lubricating-pumps
    • F16N13/20Rotary pumps

Definitions

  • the scavenge pump In order to insure removal of substantially -all the oil from thesump underall engine operating conditions, the scavenge pump isprovided with a" capacity more than. sufiicient for returning all the oil from the sump to the reservoir under the'most adverse pump operating conditions. Accordingly, the scavenge pump returns a considerable amount of air and other gases, as well as oil to the oil supply reservoir. The air and other gases become entrained within the oil and are only partially separated in the oil reservoir. This entrainment of. air and/or gases within the engine lubricating oil supplied to thev lubricating pump'consi'derably reduces the quantity of oil delivered by this pump.
  • the invention consists in the provision of a bleed from the discharge chamber of the.
  • Figure l is a schematic view of a lubrication system for an. internal combustion engine
  • Figure? is a sectional view through-"a scavenge pump used in the system of Figure 1;
  • Figure 3 is a sectional view taken along line 33 of Figure 2; and Figure l is a sectional'view of a modification.
  • a conventional radial cylinder internal combustion engine If! is'provided with'a bank of radially disposed cylinders licand an engine sump M.
  • the lubrication system of the engine comprises an oil supply tank or reservoir [6, an engine driven oil pump I8, engine drivenscavenge pumps ill-and 20, and anoil'cooler; 22;
  • Each ofthe pumps l8, l9 and 20 is' a rotary positive displacement type gear pump, e..g.., these pumps may be conventional gear-pumps comprisinga'pair of spur gears.
  • the scavenge. pump 20 is arranged to draw oil from the engine sump it andto pump the oil into the oil: supply tank it by way of lines 24 and 26, oil cooler :22, and line 28.
  • the scavenge pump 19' has a smaller capacity than the pump 20,
  • the scavenge pump 20 is made oversize. This is essential in order to prevent oil. fromoverflowing thesump into the lower cylinders of the engine.
  • the gases entrained within the oil are objecti'onable: because onlya portion of these gases 'separate'out from the oil in the oiltank and therefore the pump l8 delivers gases as well as oil, thereby reducing the quantity of lubricating oil delivered by the pump I8 to the engine.
  • the gas pressure built up in its discharge chamber tends to blow back through the pump gears, thereby stripping these gears of oil, and making it diflicult for the pump to reprime itself. This condition is aggravated in the case of the pump [9 which has a smaller capacity than the pump 20.
  • the gases delivered by the pump 20 to the Y connection between lines [9, 26 and 30 also tend to blow back through line 30 and the gears of pump [9.
  • both scavenge pumps l9 and 20 are preferably modified as i1 lustrated in the vertical pump section of Figure 2, and as further illlustrated in Figure 3.
  • Either scavenge pump comprises a casing 34, an inlet chamber 36, a discharge chamber 38, and a pair of meshing spur gears 40.
  • a bleed opening 42 is provided out through the pump casing from the vicinity of the meshing engagement of the gears at one end of the gears and on their discharge side. The exact location of this bleed opening in the vicinity of meshing engagement of the gears is not critical. This opening may be vented to the atmosphere or to any suitable space of relatively low pressure and preferably is connected back into the engine crank case through a line 44.
  • a second bleed opening may be provided through the pump casing at the other end of the discharge side of the pump gears.
  • the one or more bleed openings 42 actually open into the discharge chamber of the pump at a point in which the gear teeth are in meshing engagement.
  • a groove or recess 43 may be provided along the inner wall of the pump casing from the bleed opening 42 to a point downstream therefrom clear of the gear teeth, as illustrated.
  • the groove 43 is not essential to the function of the bleed opening 42.
  • the scavenge pumps [9 and 20 each provided with a bleed opening 42, the quantity of gases entrained in the oil returning to the supply tank It is substantially reduced. Some oil will also escape through the bleed opening 42 back into the engine crank case and sump, but this is not objectionable, since the scavenge pumps l9 and 20 are provided with a capacity considerably in excess of that normally required. Also, if either of the pumps H] or 20 should become unprimed, the gas delivered to the discharge side of this pump can readily escape through the bleeding opening 42 back into the engine crank case instead of blowing back through the pump gears, and therefore, the discharge chamber or port 38 of the pump will remain substantially full of oil, and the pump gears will run in oil, thereby keeping the pump clearances sealed.
  • bleed opening 42 operations and functions of the bleed opening 42 are the same, regardless of the orientation of the pump gears or the orientation of its inlet and outlet ports.
  • the pump gears are mounted for rotation about horizontal axes with the pump discharging downwardly, but obviously the bleed opening 42 would function just the same, even though the pump were modified so that it discharged upwardly or horizontally or if the pump gears were mounted for rotation about vertical axes.
  • the pump gears were mounted for rotation about vertical axes, then with but a single bleed opening 42, it preferably should be disposed adjacent the upper end of the gears.
  • FIG. 4 illustrates such a construction in which the pump is provided with an inlet chamber 50, an outlet chamber 52 and a pair of meshing spur gears 54. With the arrangement as illustrated in Figure 4, the gases delivered by the pump tend to collect at the upper zone of the pump discharge chamber 52.
  • a bleed opening 55 is disposed at the upper zone of the discharge chamber adjacent the upper gear 54. This opening may also be connected back into the engine crank case as in the case of the bleed opening 42. In this way, any gases collecting in the upper zone of the pump discharge chamber can readily escape through the bleed opening 56, and therefore, both pump gears will continue to run in oil while the pump is unprimed.
  • the invention has been disclosed in connection with scavenge pumps of an engine lubrication system, the invention is not so limited but is of general application. Thus, the invention can be applied to any rotary gear pump which has a capacity greater than the quantity of liquid which enters the pump, or which at times may become unprimed during operation.
  • each of said pumps comprising a pair of meshing spur gears and having a bleed opening in its discharge side in the region of meshing engagement of its gears.
  • an engine lubrication system comprising an engine, an oil supply reservoir, and an engine driven positive displacement pump, said pump comprising a housing having rotatable pumping elements mounted therein for returning oil to said reservoir from said engine, said housing having a bleed opening in its discharge side immediately adjacent to the path of rotation of said pump elements, said bleed opening communicating with the housing of said engine.
  • an engine lubrication system comprising an oil supply reservoir, an engine driven positive displacement pump, said pump comprising a housing having rotatable pumping elements mounted therein for returning oil to said reservoir from said engine, said housing having a bleed opening on its discharge side immediately adjacent to the path of rotation of said pump elements.
  • an engine driven positive displacement pump comprising a housing having a pair of meshing spur gears, said gears being rotatable to pump oil from said engine to said supply reservoir and said housing having a bleed opening on its discharge side in the region of meshing engagement of said gears.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)

Description

April 1950 w. L. WEEKS ETAL 2,503,016 I LUBRICANT SCAVENGING PUMP MEANS Filed Aug. 5, 1944 Patented Apr. 4, 1950 UNITED STATES PATENT OFFICE 'LUBRICAN T SCAVENGING PUMP MEANS Walter L. Weeks, East Wyckofi, Charles A. Stewart, Westfieldpand William H. .Holmes', Upper Montclair, N. J., assignorsto Wright Aeronautical Corporation, a corporation of New York ApplicationAugusti 5, 1944, Serial No. 548,254
ing .oil. from a-"reservoir, and'supplies it under pressure to the engine parts to be lubricated from which the oil drains into a sump, and an engine driven scavenge pump operates to return the oil from'thesump'to the. reservoir. In order to insure removal of substantially -all the oil from thesump underall engine operating conditions, the scavenge pump isprovided with a" capacity more than. sufiicient for returning all the oil from the sump to the reservoir under the'most adverse pump operating conditions. Accordingly, the scavenge pump returns a considerable amount of air and other gases, as well as oil to the oil supply reservoir. The air and other gases become entrained within the oil and are only partially separated in the oil reservoir. This entrainment of. air and/or gases within the engine lubricating oil supplied to thev lubricating pump'consi'derably reduces the quantity of oil delivered by this pump.
It isan' object of this invention to provide means for removing at least a portion of the air and/0r gases delivered by the engine driven scavenge pump or pumps. It is a further object of this invention to prevent the formation of large gas pressures in the discharge chamber of the pump in the event the pump becomes unprimed since this gas pressure may blow back through the pump to strip the pump clearances of oil, thereby rendering it difficult for the pump to reprimeitself. The invention consists in the provision of a bleed from the discharge chamber of the.
scavenge pump and through which the air and/or other gases delivered. by the pump can escape, thereby reducingthe quantity of gases entrained within the-oil. In addition, because the gases can escape from the discharge chamber through this bleed, the discharge chamber remainsJsubstantially full of oil, even though the pump 'becomes unprimed, and therefore, the pump clearances will remain sealed and the pump will'rea'di-ly reprime itself, when oil is'again available. Al-
though the invention is disclosed in'connection with a lubrication system of an'aircraft engine, it obviously is of general application, and can be used with any. gear pump which has. a capacity greater than the rate at which liquid enters the" 55 pump or to. any suchpump which may becomeunprimetd.
Qther objects "of the invention will becomeapparent upon'ireading the annexed detailed description in connection with the drawing in which:
.Figure l is a schematic view of a lubrication system for an. internal combustion engine;
Figure? is a sectional view through-"a scavenge pump used in the system of Figure 1;
Figure 3 is a sectional view taken along line 33 of Figure 2; and Figure l is a sectional'view of a modification.
Referring tothe drawing, a conventional radial cylinder internal combustion engine If! is'provided with'a bank of radially disposed cylinders licand an engine sump M. The lubrication system of the engine comprises an oil supply tank or reservoir [6, an engine driven oil pump I8, engine drivenscavenge pumps ill-and 20, and anoil'cooler; 22; Each ofthe pumps l8, l9 and 20is' a rotary positive displacement type gear pump, e..g.., these pumps may be conventional gear-pumps comprisinga'pair of spur gears. The scavenge. pump 20 is arranged to draw oil from the engine sump it andto pump the oil into the oil: supply tank it by way of lines 24 and 26, oil cooler :22, and line 28. The scavenge pump 19' has a smaller capacity than the pump 20,
' and operates to pump oil from the rear engine section 29 to the oil supply tank "5 by way of lines 30 and 26, oil cooler 22, and line 28. A linetl connects the inlet side of the pump l8 to the bottom of the oil tank, and this pump delivers oil under pressure to the various bearing surfaces'of the engine through passages suchas 32. In order to insure substantially complete removal of allltheoil from the engine sump under all operating conditions, the scavenge pump 20 is made oversize. This is essential in order to prevent oil. fromoverflowing thesump into the lower cylinders of the engine. The result isthat' only part of'the capacity'of the scavenge pump 2liisieffective for pumping oil back into the oil tanlntheremainder of the capacityof the pump being effective 'to pump air or other gasesinto the oil "tank. Similarly, the capacity of "the scavenge: pump I9" is in excess of its normal requirement, and therefore, a considerable quantity of gases becomes entrained within the oil returned to the tank It. 'Thestructure sofar described. is quite conventional.
The gases entrained within the oil are objecti'onable: because onlya portion of these gases 'separate'out from the oil in the oiltank and therefore the pump l8 delivers gases as well as oil, thereby reducing the quantity of lubricating oil delivered by the pump I8 to the engine. Also, when, for example, pump H! or becomes unprimed, the gas pressure built up in its discharge chamber tends to blow back through the pump gears, thereby stripping these gears of oil, and making it diflicult for the pump to reprime itself. This condition is aggravated in the case of the pump [9 which has a smaller capacity than the pump 20. Thus, when the pump [9 becomes unprimed, the gases delivered by the pump 20 to the Y connection between lines [9, 26 and 30 also tend to blow back through line 30 and the gears of pump [9.
To overcome these difiiculties, both scavenge pumps l9 and 20 are preferably modified as i1 lustrated in the vertical pump section of Figure 2, and as further illlustrated in Figure 3. Either scavenge pump comprises a casing 34, an inlet chamber 36, a discharge chamber 38, and a pair of meshing spur gears 40. A bleed opening 42 is provided out through the pump casing from the vicinity of the meshing engagement of the gears at one end of the gears and on their discharge side. The exact location of this bleed opening in the vicinity of meshing engagement of the gears is not critical. This opening may be vented to the atmosphere or to any suitable space of relatively low pressure and preferably is connected back into the engine crank case through a line 44.
With this arrangement, upon operation of the pump, the region of the bleed opening 42 is primarily occupied by the gases delivered by the pump, the relatively heavy oil being thrown away from this region by the gears 40. As a result, a substantial portion of the gases delivered by the pump escapes through the bleed opening 42. At this point it should be noted that if desired, a second bleed opening may be provided through the pump casing at the other end of the discharge side of the pump gears. Preferably the one or more bleed openings 42 actually open into the discharge chamber of the pump at a point in which the gear teeth are in meshing engagement. Then, in view of the trapping action of the meshing gear teeth, a high pressure is built up between these gear teeth forcing the gases out from between the teeth through the bleed opening or openings 42. Also, in order to further facilitate the escape of the gases delivered by the pump through the bleed opening 42, a groove or recess 43 may be provided along the inner wall of the pump casing from the bleed opening 42 to a point downstream therefrom clear of the gear teeth, as illustrated. However, the groove 43 is not essential to the function of the bleed opening 42.
With the scavenge pumps [9 and 20 each provided with a bleed opening 42, the quantity of gases entrained in the oil returning to the supply tank It is substantially reduced. Some oil will also escape through the bleed opening 42 back into the engine crank case and sump, but this is not objectionable, since the scavenge pumps l9 and 20 are provided with a capacity considerably in excess of that normally required. Also, if either of the pumps H] or 20 should become unprimed, the gas delivered to the discharge side of this pump can readily escape through the bleeding opening 42 back into the engine crank case instead of blowing back through the pump gears, and therefore, the discharge chamber or port 38 of the pump will remain substantially full of oil, and the pump gears will run in oil, thereby keeping the pump clearances sealed. These operations and functions of the bleed opening 42 are the same, regardless of the orientation of the pump gears or the orientation of its inlet and outlet ports. As illustrated in Figure 2, the pump gears are mounted for rotation about horizontal axes with the pump discharging downwardly, but obviously the bleed opening 42 would function just the same, even though the pump were modified so that it discharged upwardly or horizontally or if the pump gears were mounted for rotation about vertical axes. However, if the pump gears were mounted for rotation about vertical axes, then with but a single bleed opening 42, it preferably should be disposed adjacent the upper end of the gears.
With the pump arranged to discharge horizontally and with the pump gears mounted for rotation about vertically spaced horizontal axes, it is also desirable to locate a bleed opening at the upper zone of the pump discharge chamber adjacent to the upper gear either in addition to or in lieu of the bleed opening provided adjacent the meshing zone of the gears. Figure 4 illustrates such a construction in which the pump is provided with an inlet chamber 50, an outlet chamber 52 and a pair of meshing spur gears 54. With the arrangement as illustrated in Figure 4, the gases delivered by the pump tend to collect at the upper zone of the pump discharge chamber 52. Therefore, when the pump became unprimed, these gases, under the pump back pressure, would tend to blow back through the upper gear 54, thereby tending to strip this gear of oil and making it diflicult for the pump to reprime itself. To overcome this difficulty, a bleed opening 55 is disposed at the upper zone of the discharge chamber adjacent the upper gear 54. This opening may also be connected back into the engine crank case as in the case of the bleed opening 42. In this way, any gases collecting in the upper zone of the pump discharge chamber can readily escape through the bleed opening 56, and therefore, both pump gears will continue to run in oil while the pump is unprimed.
Although the invention has been disclosed in connection with scavenge pumps of an engine lubrication system, the invention is not so limited but is of general application. Thus, the invention can be applied to any rotary gear pump which has a capacity greater than the quantity of liquid which enters the pump, or which at times may become unprimed during operation.
While we have described our invention in detail in its present preferred embodiment, it will be obvious to those skilled in the art, after understanding our invention, that various changes and modifications may be made therein without departing from the spirit or scope thereof. We aim in the appended claims to cover all such modifications and changes.
We claim as our invention:
1. In an engine lubrication system comprising an oil supply reservoir and a pair of engine driven scavenge pumps for returning oil through a common conduit to said reservoir, each of said pumps comprising a pair of meshing spur gears and having a bleed opening in its discharge side in the region of meshing engagement of its gears.
2. In an engine lubrication system comprising an engine, an oil supply reservoir, and an engine driven positive displacement pump, said pump comprising a housing having rotatable pumping elements mounted therein for returning oil to said reservoir from said engine, said housing having a bleed opening in its discharge side immediately adjacent to the path of rotation of said pump elements, said bleed opening communicating with the housing of said engine.
3. In an engine lubrication system comprising an oil supply reservoir, an engine driven positive displacement pump, said pump comprising a housing having rotatable pumping elements mounted therein for returning oil to said reservoir from said engine, said housing having a bleed opening on its discharge side immediately adjacent to the path of rotation of said pump elements.
4. In an engine lubrication system comprising an oil supply reservoir, an engine driven positive displacement pump comprising a housing having a pair of meshing spur gears, said gears being rotatable to pump oil from said engine to said supply reservoir and said housing having a bleed opening on its discharge side in the region of meshing engagement of said gears.
WALTER L. WEEKS. CHARLES A. STEWART. WILLIAM H. HOLMES.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS
US548254A 1944-08-05 1944-08-05 Lubricant scavenging pump means Expired - Lifetime US2503016A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US548254A US2503016A (en) 1944-08-05 1944-08-05 Lubricant scavenging pump means

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US548254A US2503016A (en) 1944-08-05 1944-08-05 Lubricant scavenging pump means

Publications (1)

Publication Number Publication Date
US2503016A true US2503016A (en) 1950-04-04

Family

ID=24188036

Family Applications (1)

Application Number Title Priority Date Filing Date
US548254A Expired - Lifetime US2503016A (en) 1944-08-05 1944-08-05 Lubricant scavenging pump means

Country Status (1)

Country Link
US (1) US2503016A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2578275A (en) * 1949-09-30 1951-12-11 Irvin R Whiteman Air-free lubricant pump discharge system
US2697402A (en) * 1950-09-15 1954-12-21 Arthur E Lindquist Impeller construction for rotary pressure pumps
US3212449A (en) * 1963-08-13 1965-10-19 Borg Warner Fuel injection system
US3817668A (en) * 1969-05-28 1974-06-18 K Mayer Gear wheel pump with feed passage of constant hydraulic cross section
US4683984A (en) * 1985-10-03 1987-08-04 Sundstrand Corporation Scavenge oil system
US4846308A (en) * 1987-01-28 1989-07-11 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Liquid feed pump system
US5004407A (en) * 1989-09-26 1991-04-02 Sundstrand Corporation Method of scavenging air and oil and gear pump therefor
US12083848B1 (en) 2023-05-15 2024-09-10 DRiV Automotive Inc. Single axle roll control system with dual impeller pump arrangement
US12083851B1 (en) 2023-05-15 2024-09-10 DRiV Automotive Inc. Single axle roll control system with multiple circuit-specific pressurizing devices

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1485537A (en) * 1918-01-14 1924-03-04 Packard Motor Car Co Hydrocarbon motor
GB493553A (en) * 1937-04-13 1938-10-11 John Stanley Orme Lubrication systems for engines
US2140735A (en) * 1935-04-13 1938-12-20 Henry R Gross Viscosity regulator
US2223112A (en) * 1938-10-26 1940-11-26 Martin & Schwartz Inc Apparatus for pumping and separating gas and liquid bodies
US2229231A (en) * 1939-02-25 1941-01-21 Holland Furnace Co Fuel pump
US2246951A (en) * 1938-02-15 1941-06-24 Aqua Systems Inc Pump unit for liquid dispensing apparatus
FR880952A (en) * 1941-12-02 1943-04-12 Improvements to the method of preheating the lubricating oil on internal combustion engines
US2316729A (en) * 1941-06-30 1943-04-13 Napler & Son Ltd D Tank for use in aircraft
US2362724A (en) * 1941-03-08 1944-11-14 Phillips Petroleum Co Liquefied petroleum gas dispensing system
US2443875A (en) * 1943-03-13 1948-06-22 Avco Mfg Corp Lubricating system for engines

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1485537A (en) * 1918-01-14 1924-03-04 Packard Motor Car Co Hydrocarbon motor
US2140735A (en) * 1935-04-13 1938-12-20 Henry R Gross Viscosity regulator
GB493553A (en) * 1937-04-13 1938-10-11 John Stanley Orme Lubrication systems for engines
US2246951A (en) * 1938-02-15 1941-06-24 Aqua Systems Inc Pump unit for liquid dispensing apparatus
US2223112A (en) * 1938-10-26 1940-11-26 Martin & Schwartz Inc Apparatus for pumping and separating gas and liquid bodies
US2229231A (en) * 1939-02-25 1941-01-21 Holland Furnace Co Fuel pump
US2362724A (en) * 1941-03-08 1944-11-14 Phillips Petroleum Co Liquefied petroleum gas dispensing system
US2316729A (en) * 1941-06-30 1943-04-13 Napler & Son Ltd D Tank for use in aircraft
FR880952A (en) * 1941-12-02 1943-04-12 Improvements to the method of preheating the lubricating oil on internal combustion engines
US2443875A (en) * 1943-03-13 1948-06-22 Avco Mfg Corp Lubricating system for engines

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2578275A (en) * 1949-09-30 1951-12-11 Irvin R Whiteman Air-free lubricant pump discharge system
US2697402A (en) * 1950-09-15 1954-12-21 Arthur E Lindquist Impeller construction for rotary pressure pumps
US3212449A (en) * 1963-08-13 1965-10-19 Borg Warner Fuel injection system
US3817668A (en) * 1969-05-28 1974-06-18 K Mayer Gear wheel pump with feed passage of constant hydraulic cross section
US4683984A (en) * 1985-10-03 1987-08-04 Sundstrand Corporation Scavenge oil system
US4846308A (en) * 1987-01-28 1989-07-11 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Liquid feed pump system
US5004407A (en) * 1989-09-26 1991-04-02 Sundstrand Corporation Method of scavenging air and oil and gear pump therefor
US12083848B1 (en) 2023-05-15 2024-09-10 DRiV Automotive Inc. Single axle roll control system with dual impeller pump arrangement
US12083851B1 (en) 2023-05-15 2024-09-10 DRiV Automotive Inc. Single axle roll control system with multiple circuit-specific pressurizing devices

Similar Documents

Publication Publication Date Title
US2178662A (en) Fluid compressor
US3763960A (en) Lubricating system for internal combustion engines
US3669579A (en) Compressors
US3291385A (en) Receiver-separator unit for liquidinjected compressor
GB1150021A (en) Lubrication System for Gas Turbine Engines
US2440815A (en) Crankcase construction
US2888097A (en) Lubrication system
US2956730A (en) Jet ejector lubricant return means for a refrigeration compressor
US2503016A (en) Lubricant scavenging pump means
US3936249A (en) Rotary compressor of oil cooling type with appropriate oil discharge circuit
EP0460578A1 (en) Screw fluid machine
US2988267A (en) Rotary compressor lubricating arrangement
US2274942A (en) Lubricated refrigerant compressor
GB994325A (en) Bearing lubrication system for meshing-screw compressors
US2739758A (en) Rotary compressor
US2038131A (en) Lubricating system for compressors
US2846138A (en) Refrigeration compressor
US1876708A (en) Crank case construction for engines and the like
US2937715A (en) Lubrication system for gas compressor
US3698515A (en) Vacuum pump lubrication system
US2606715A (en) Lubricating system for rotary pumps
US3606935A (en) Lubricating system for internal combustion engines
US2522638A (en) Gas compressing apparatus
US2714428A (en) Accessory gear drive lubricating means
US3123287A (en) figure